Entry Trajectory Optimization by Second-Order Cone Programming
Author:
Affiliation:
1. School of Aeronautic Science and Engineering, Beihang University, 100191 Beijing, People’s Republic of China
2. Department of Aerospace Engineering, Iowa State University, Ames, Iowa 50011-2271
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.G001210
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1. Convex Programming Approach to Powered Descent Guidance for Mars Landing
2. Minimum-Landing-Error Powered-Descent Guidance for Mars Landing Using Convex Optimization
3. Lossless convexification of a class of optimal control problems with non-convex control constraints
4. Lossless Convexification of Nonconvex Control Bound and Pointing Constraints of the Soft Landing Optimal Control Problem
5. Maximum Divert for Planetary Landing Using Convex Optimization
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